Flexible flaps for separation control on a wing with low aspect ratio
bionics pilot project:
main objective:
Brown Skua with “eddy-flaps”
aerofoil with eddy- flaps
goal:
research goal
experimental setup at the wind tunnel
porosity
aerofoil with silk flaps
silk flaps
polar diagram for ‘perforated plastic sheet’ flaps
aerofoil for pressure distribution
pressure distribution at 16 degrees
pressure distribution at 19 degrees
flow visualisation
pressure distribution at 36 degrees
polar diagram (calculated from all measuring rows)
lift distribution without flaps at different angles of attack
lift distribution with flaps at different angles of attack
summary:
E-Mail: patone@fb10.tu-berlin.de
Homepage: http://www.bionik.tu-berlin.de/user/giani/giani.html
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